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Propulsion System of Boeing 747
Group Members:
Shamsuddin
Mustazly
Hidayat
Pearl
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What is Boeing 747?
Also know as B-747 or B747
Used for crossing oceans
Double decked plane
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Exterior View
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Interior View
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Cross Section View
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TURBOFAN
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What is Turbofan ?
Designed as a compromised between the
turboprop (fuel efficient but noisy) and turbojet
(powerful yet thirsty)
Has large internal propeller or ducted fan and two
streams of air flowing in the engine.
Main stream goes into all of the components like a
turbojet
The secondary flow passes through the fan and is
either ducted through a second nozzle or mixed
back with the main stream leaving the turbine.
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Can be classified as:
Mixed or unmixed
Low or high by passSingle, two or three spool
With or without after burning
Geared or ungeared
Nuclear of non-nuclear
Characteristics:
Widely used today
Capable of medium to high thrust
Capable of supersonic speed
Better fuel efficiency
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THE WORKING
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1. The fan will suck the air into compressor.
2. The compressor will squeeze and compress the air.
3. The air will be mixed with oil and burn inside the combustion chamber.
4. The air will be force out into the turbine and power the turbine to rotate.
5. The turbine will power the compressor to rotate.
6. The air will be blown outside the nozzle.
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Animation of a 2-spool, high-bypass
turbofan.A. Low pressure spool
B. High pressure spool
C. Stationary components
1. Nacelle
2. Fan
3. Low pressure compressor4. High pressure compressor
5. Combustion chamber
6. High pressure turbine
7. Low pressure turbine
8. Core nozzle
9. Fan nozzle
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Type of engines
High bypassLow bypass
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Engine Series
General Electric (GE)
CF6 - Type of engine: High bypass turbofan
- Thrust range : 40,000 - 72,000 lbs.
- Introduction : 1971
Rolls Royce
RB211-524 - Type of engine: High bypass turbofan
- Thrust range: 37,400 - 60,600lbs
- Introduction: 1997
Pratt & Whitney
JT9D-7 - Type of engine: High bypass turbofan
- Thrust range: 46,300 - 50,000 lbs
- Introduction: 1970
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1. Horsepower of 1 Engine125,000hp
3. Average altitude35,00037,000 feet
2. Maximum altitude45,100 feet
4. How far can B747 fly?7,260 nm
(13,450km)
5. How long can B747 fly? 16 to 19 hours
with fuel saving6. How far can B747 glide without fuel?
- At Altitude 42,000 ft136 miles
- At Sea Level100miles
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7. Only B747-400 from B747 family have afterburner.
8. Life span of an B747 aircraft- Average 25 to 30 years (large number of cycles)
** Others - 20 years (small number of cycles)
9. B747s engines are mixed nozzle
10. The 747-400 was touted as the fastest subsonic
commercial airliner in service (913km/h).- Cruised at 0.85 Mach (85 % of the speed of sound)
- Pratt & Whitney, generated the most powerful 747-
400 engine with 63,300 lb (28,712 kg) thrust each
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Die!!!!
Hahaha..
Just kidding ^^
Still able to proceed
to your destination
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Why?
Alight 747 can stay with only two engines, but
not a heavy one. The one engine is needed to
power the hydraulics.
Which mean a B747 still able to fly with 3
engines.
Thenwhy need 4 engines??Backup
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Model Certification First Airline in service Last Delivery747-100/SR/B 30/12/69 Pan Am 9/86
Japan Air Lines
747-200 23/12/70 KLM 12/90USAF747-200F 03/07/72 Lufthansa 11/91
Nippon Cargo
747-200C 24/07/73 World Airways 9/88Martinair
747SP 04/02/76 Pan Am 12/09/89Abu Dhabi Govt.
747-200M 03/07/75 Air Canada12/09/89 -
Abu Dhabi Govt. (UAE)
747-300M 03/05/83 Swissair 9/90Sabena
747-300/SR 03/07/83 Swissair 10/88Japan Asia
747-400 01/10/89 Northwest747-400M 01/10/89 KLM 04/10/02
KLM
747-400D 10/10/91 Japan Air Lines 12/95All Nippon Airways
747-400F 22/10/93 Cargolux 5/7/09Nippon Cargo Airlines
747-400ER 29/10/02 Qantas 7/30/03Qantas
747-400ERF `16/10/02 Air France 11/10/09LoadAir Cargo
747-8F 19/08/11 Cargolux747-8 14/12/12 Lufthansa
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ENGINE TYPE
Pratt & Whitney (PW)
General Electric (GE)
Rolls-Royce (RR)
ENGINE MODEL
PW JT9D-7A/-7F/-7J
RR RB211-524B2
GE CF6-45A2 (747SR)
ENGINE SPEC
Max speed : 967km/h(522knot) ; Mach 0.89
Cruising speed :907km/h (490knot) ;Mach 0.84
Engine thrust :
PW 46,500 lbf, (207kN),
RR 50,100 lbf, (223 kN)
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ENGINETYPE
Pratt & Whitney
(PW)
General Electric(GE)
Rolls-Royce (RR)
ENGINEMODEL
PW
JT9D-7R4G2
GE
CF6-50E2
RR
RB211-524D4
ENGINESPEC
Max speed : 967km/h(522knot) ; Mach 0.89
Cruising speed : 907km/h(490knot) ; Mach 0.84
Engine thrust :
PW 54,750 lbf (244 kN)
GE 52,500 lbf (234 kN)
RR 53,000 lbf (236 kN)
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ENGINE TYPE
ENGINE MODEL
ENGINE SPEC
Pratt & Whitney (PW)
General Electric (GE)
Rolls-Royce (RR)
PW JT9D-7R4G2
GE CF6-80C2B1
RR RB211-524D4
Max speed : 967km/h (522knot) ; Mach0.89
Cruising speed : 907km/h (490knot) ;Mach 0.84
Engine thrust :
PW 54,750 lbf (244 kN)
GE 55,640 lbf (247 kN)
RR 53,000 lbf (236 kN)
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ENGINE TYPE
Pratt & Whitney (PW)
General Electric (GE)
Rolls-Royce (RR)
ENGINE MODEL
PW 4062
GE CF6-80C2B5F RR RB211-524G/H
ENGINE SPEC
Max speed : 988 km/h
(533 knots) ; Mach 0.85
Cruising speed : 912km/h
(493knots); Mach 0.92
Engine thrust :
PW 63,300 lbf (282 kN)
GE 62,100 lbf (276 kN)
RR 59,500/60,600lbf
(265/270 kN)
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EN
GINETY
PE
GeneralElectric (GE)
ENG
INEMOD
EL
GEnx-2B67
EN
GINESP
EC
66,500 lbf(296 kN)
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References Ronald D.Flackn, Fundamentals of Jet Propulsion with
Application, Cambridge Aerospace Series, 2005. Thomas A. Ward, Aerospace propulsion Systems,John
Wiley & Sons (Asia) Pte Ltd, 2010
http://www.boeing.com/boeing/commercial/747family/pf/pfdomestic_prod.page
http://wiki.answers.com/Q/Average_flying_height_for_a_Being_747_in_miles#slide4
http://www.pw.utc.com/JT9D_Engine
http://www.rolls-royce.com/civil/products/largeaircraft/rb211_524/
http://www geaviation com/